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Frontier Limitations > Limittations > Flashcards

Limittations Flashcards

1
Q

What is the approach category of the A319, A320, and A321?

A

319 & 320 category C
321 category D

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2
Q

What is Frontier’s stabilized approach policy?

A

STABILIZED APPROACH POLICYStabilization Criteria1000 ft Steady rate of descent not to exceed 1,200 FPM. On the correct lateral path (“Course”); (± one dot for ILS/LOC, 0.30 NM cross track for RNAV, or 1/2 dot for VOR)*On the correct vertical path (“Glidepath”); (± one dot)In the final landing configuration (Landing Gear and Flaps Extended)Absent any GPWS Warnings and Cautions Criteria 500ft Steady rate of descent not to exceed 1,000 FPMXWithin -5 to +15 knots of target speed for approach, thrust stabilized usually above idle

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3
Q

Maximum Operational Pressure Altitude

A

39800

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4
Q

Maximum Pressure Altitude for Takeoff & Landing

A

9200

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5
Q

Minimum Pressure Altitude for Takeoff & Landing

A

-2000ft

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6
Q

Runway slope (mean)

A

+-2%

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7
Q

Minimum runway width

A

AC 221, 227, 228,229 100ft
All other AC 148ft

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8
Q

Maximum crosswind takeoff & landing

A

Takeoff 35kts landing 38kts

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9
Q

Maximum tailwind

A

319 & 320, 321 Neo takeoff 15kts landing 10kts
321CEO takeoff 10kts landing 10kts

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10
Q

MAXIMUM WIND FOR PASSENGER DOOR OPERATION

A

65kts

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11
Q

MAXIMUM WIND FOR CARGO DOOR OPERATIONS

A

40/50kts

If the aircraft nose is oriented into the wind, or if the cargo door is on the leeward side of the aircraft, operation of the cargo door is permitted in winds up to 50 knots. If wind speed begins to exceed these limitations, the cargo door must be closed before the wind speed exceeds 65 kts.

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12
Q

VMO/MMO

A

350/.82

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13
Q

RECOMMENDED TURBULENT AIR PENETRATION SPEED

A

319&320
Below FL 200 250kts
FL 200-310 275kts
Above FL 310 .76

321
Below FL200 270kts
FL 200-310 300kts
Above FL310 .76

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14
Q

LANDING GEAR SPEED – MAXIMUM

A

Retraction VLO 220kts
Extension VLO 250kts
Extended VLE 280kts

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15
Q

Tire Speed
Maximum Ground Speed

A

195kts

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16
Q

WINDSHIELD WIPER OPERATION
Max speed

A

230kts

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17
Q

COCKPIT WINDOW - OPEN
Max speed

A

200kts

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18
Q

TAXI SPEED Weight greater than 167,550 lbs

A

20kts in a turn

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19
Q

PRESSURIZATION – CABIN DIFFERENTIAL
Negative
Positive
Safety relief valve

A

Negative -1.0 psi
Positive 9.0 psi
Safety relief valve 8.6 psi

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20
Q

APU BLEED USE WITH HIGH PRESSURE (HP) GROUND UNIT

A

Prohibited

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21
Q

AVIONICS VENTILATION The aircraft electrical system should not be powered for more than 2 hours without a cooling system when the outside air temperature is above

A

49 degrees

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22
Q

The APU may be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed. Maintenance action is required within the next __hours of APU operation.

A

10

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23
Q

APU STARTER DUTY CYCLE

A

Between each start attempt 1 minute
After 3 consecutive start attempts 60 minutes

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24
Q

APU EGT AND ROTOR SPEED

A

Maximum EGT 675C
Maximum EGT for start At or Above 35,000ft 1120C
Below 35,000ft 1090C

Maximum rotor speed 107%

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25
Q

During refuel/defuel procedures, APU starts or shutdown are permitted with the following restrictions:

A

If the APU failed to start or following an automatic APU shutdown, do not start the APU. If a fuel spill occurs, perform a normal APU shutdown.

26
Q

What is the maximum altitude to start the APU using battery power only (Elec Emerg Config)?

A

25,000ft

27
Q

What is the autopilot minimum engagement height after takeoff (if SRS is indicated)?

A

100ft AGL

28
Q

What is the autopilot minimum engagement height enroute?

A

900ft AGL

29
Q

At what height must the autopilot be turned off for an RNAV VISUAL APPROACH?

A

500ft AGL

30
Q

At what height must the autopilot be turned off for Non-Precision Approaches?

A

DDA/DA

31
Q

At what height must the autopilot be turned off for a Non-Autoland ILS with CAT 1 FMA?

A

160 AGL

32
Q

At what height must the autopilot be turned off for a Non-Autoland ILS with CAT 2/3 FMA?

A

80 AGL

33
Q

What is the minimum height the autopilot can be engaged during a GO-Around (If SRS is indicated)?

A

100AGL

34
Q

When must the autopilot be turned off after an autoland approach?

A

Rollout taxi speed

35
Q

When is an autoland required?

A

Below CAT 1 Minimums

36
Q

What is the minimum engine oil quantity required prior to each flight?

A

CEO Aircraft 9.5 qt +.5 qt per every hour of estimated flight time
NEO Aircraft 9.0 qt +.5 qt per every hour of estimated flight time and not below 10.6 qt
321 NEO OAT at or above -30C 14qt. At or below -30 16.5qt

37
Q

What is the minimum engine oil temperature required before takeoff?

A

19C

38
Q

What is the maximum time limit to use TOGA thrust with all engines operating? How about if one engine is inoperative?

A

5 min all engines
10 min single engine

39
Q

Takeoff at reduced thrust is prohibited when?

A

On slippery or contaminated runways; When suspected, reported, or known windshear is present (e.g., predictive windshear alerts, or ATC-issued windshear alerts for the departure runway or departure path); When a Special Departure Procedure specifies full thrust for takeoff.

40
Q

What is the maximum altitude that the Flaps or Slats may be extended?

A

20,000ft

41
Q

What are the flight maneuvering load acceleration limits?

A

Clean configuration. -1.0g to +2.5g
Other configurations slats/flaps extended 0.0g to +2.0g

42
Q

What is the max altitude to use the APU to supply electrical power with one pack operating?

A

22,500ft

43
Q

What is the max altitude for an APU start using normal electrics?

A

39,000ft

44
Q

What is the max altitude to use the APU for an engine start?

A

20,000ft

45
Q

What is the max altitude to use the APU to supply electrical power with both packs operating?

A

15,000ft

46
Q

Is the use of APU bleed air for wing anti-ice permitted?

A

No

47
Q

The use of AP or FD in ____ ___or _____ mode is not permitted inside the FAF or below 1000 ft AGL on a visual approach?

A

Open DES or DES

48
Q

Autolands are not authorized on runways less than ____ feet wide?

A

150ft

49
Q

Autolands are approved for CONF 3 and CONF FULL. What configuration is recommended for all autolands in order to maximize forward slant range visibility?

A

CONF FULL

50
Q

Autolands are prohibited if braking action is reported less than _______?

A

Medium

51
Q

What conditions must be satisfied to conduct an autoland approach?

A

CAT II/III runway • CAT II/III aircraft • CAT II/III trained crew • Appropriate ground facilities operational • Wind within limits • Braking action medium or better

52
Q

If one or more of the autoland requirements cannot be met, may an approach still be conducted if the weather is below ½ mile or 2400 RVR?

A

Yes. If one of the autoland requirements cannot be met (e.g. strong crosswind), a non-autoland CAT I approach may be conducted down to our lowest authorized CAT I minimums (i.e., 1800 RVR or as published).

53
Q

Should you perform an autoland at KCOS in an A321? KCOS airport elevation is 6187 feet.

A

319&320 AC 9200ft demonstrated
321 AC 5,750ft demonstrated

54
Q

When should you use LOW vs. Medium autobrakes for an autoland? Are autobrakes required for all CAT III approaches?

A

Runway less than 8000ft medium
Runway more than 8000ft low to medium

55
Q

What are the autoland wind limitations? Note: These limitations are also located on the CAT II/III briefing card.

A

320&321 AC
Headwind 30, crosswind 15, tailwind 10, wind correction 5 to 15

321 NEO
Headwind 15, crosswind 10, tailwind 10, wind correction 5 to 15

56
Q

What is the minimum oil temp. to start the engines?

A

-40C

57
Q

What are the engine starter duty cycle limitations?

A

A320 NEO
1 and 2 cycles 60 secs off 3rd cycle 15 minutes off. stater reengagement 63%N2
A319, A320&A320 CEO
1,2,and 3 cycles 20 secs off 4th cycle 15 minutes off. Stater reengagement 20%N2

58
Q

What is the minimum fuel for takeoff?

A

3,300lbs

59
Q

Is takeoff with center tank fuel supplying the engines permitted?

A

It is prohibited

60
Q

Is taxi with deflated tires permitted?

A

Yes, given certain conditions are satisfied. However, taxiing the aircraft with deflated tires should only be done if absolutely necessary and all other means of moving the aircraft have been exhausted. Ref. FOM VOL. II, Section 2.10 for details.

61
Q

When might you consider inhibiting the ROPS function?

A

A/C 394-399 & 601-699
The ROPS function may be inhibited for a specific approach procedures which have previously been identified as potentially producing undue ROW alerts.
A/C 389-393
When a runway is identified as incompatible with ROPS by Crew briefing item or AIP, the ROPS may be inhibited when the aircraft position is less than 15NM from airfield when:

  • for a specific approach procedures which have previously been identified as potentially producing undue ROW alerts.
  • if a NOTAM displaces the landings threshold (shortened landing distance available).
62
Q

How do you inhibit the ROPS function

A

A/C 394-399 & 601-699
ROW/ROP pb-sw set to off on SURV panel
A/C 389-393
TERR pb set to off on GPWS panel

Frontier Limitations (55 decks)

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